CZ-1-3
Gross Mass: 2,050 kg (4,510 lb). Empty Mass: 250 kg (550 lb). Thrust (vac): 180.991 kN (40,688 lbf). Isp: 254 sec. Burn time: 38 sec. Propellants: Solid. Diameter: 0.77 m (2.52 ft). Span: 0.77 m (2.52 ft). Length: 3.95 m (12.95 ft). Country: China. No Engines: 1. Engine: GF-02. Status: Out of production. Cost $ : 0.300 million. First Flight: 1969. Last Flight: 2002. No Launched: 4.

Used on Launch Vehicles:  
 
 
 
 
 
 
 
 
Contact us with any corrections, additions, or comments.
Conditions for use of drawings, pictures, or other materials from this site..
To contact astronauts or cosmonauts.

© Mark Wade, 1997 - 2007 except where otherwise noted.
  
Encyclopedia Astronautica
 topic index
0 - A - B - C - D - E - F - G - H - I - J - K - L - M - N - O - P - Q - Ra - Re - Sa - Sf - Sp - T - U - V - W - X - Y - Z